Analysis of transonic flow past cusped airfoil trailing edge

Result code in IS VaVaI

<a href="https://www.isvavai.cz/riv?ss=detail&h=RIV%2F68407700%3A21220%2F15%3A00235334" target="_blank" >RIV/68407700:21220/15:00235334 - isvavai.cz</a>

Result on the web

<a href="http://dx.doi.org/10.14311/AP.2015.55.0193" target="_blank" >http://dx.doi.org/10.14311/AP.2015.55.0193</a>

DOI - Digital Object Identifier

<a href="http://dx.doi.org/10.14311/AP.2015.55.0193" target="_blank" >10.14311/AP.2015.55.0193</a>

Result language

angličtina

Original language name

Analysis of transonic flow past cusped airfoil trailing edge

Original language description

In order to verify the limits of theoretical design methods, a transonic flow past two designed cusped airfoils is numerically solved and studied. The achieved results are compared with the theoretical predictions and then analyzed in terms of flow behavior and oblique shocks formation using known classical gas dynamics relations. The regions around the sharp trailing edges are studied in detail and parameters of shock waves are solved and compared using the classical shock polar approach and verified by reduction parameters for symmetric configurations. Czech Technical University in Prague, 2015.

Czech name

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Czech description

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Type

J_x - Unclassified - Peer-reviewed scientific article (Jimp, Jsc and Jost)

CEP classification

JU - Aeronautics, aerodynamics, aeroplanes

OECD FORD branch

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Project

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Continuities

S - Specificky vyzkum na vysokych skolach

Publication year

2015

Confidentiality

S - Úplné a pravdivé údaje o projektu nepodléhají ochraně podle zvláštních právních předpisů

Name of the periodical

Acta Polytechnica

ISSN

1210-2709

e-ISSN

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Volume of the periodical

55

Issue of the periodical within the volume

3

Country of publishing house

CZ - CZECH REPUBLIC

Number of pages

6

Pages from-to

193-198

UT code for WoS article

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EID of the result in the Scopus database

2-s2.0-84936063393